To solve approach and landing problem of variable configuration reusable launch vehicle( RLV) with multi-control surfaces,a design method of approach and landing trajectory was proposed. The landing trajectory was divided into steep glide landing trajectory and flare landing trajectory. The controllable deflection limit of the aerodynamic surfaces and deep downturn quasi equilibrium equation constraints were considered and the steep glide landing trajectory optimization design was carried out. The RLV aerod...
【基金】
总装预研重点项目(9140A25030109HK0103)
【更新日期】
2016-01-13
【分类号】
V323;V249
【正文快照】
网络出版地址:www.cnki.net/kcms/detail/11.2625.V.20150521.1453.004.html引用格式:郝现伟,王勇,杨业,等.变构型多操纵面RLV进场着陆轨迹优化设计[J].北京航空航天大学学报,2015,41(12):2232-2239.Hao X W,Wang Y,Yang Y,et al.Optimization design of approach and landing
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